Three Dimensional Simulation of Supersonic Flow over Missiles of Different Shapes

In this work, a three-dimensional primitive variable of supersonic flow over missiles was computed based on finite difference computational fluid dynamic methods. The problem was considered is to deal with external, inviscid, compressible supersonic- flow over three-dimensional missiles with and wit...

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Bibliographic Details
Main Authors: Jalal M. Jalil, Hussain H. Al-Kayiem, Ahmed Kadhim Hussein
Format: Article
Language:English
Published: Unviversity of Technology- Iraq 2012-01-01
Series:Engineering and Technology Journal
Subjects:
Online Access:https://etj.uotechnology.edu.iq/article_25868_d965973c5a6c592c2ba49c03a4514202.pdf